Airfoil database search
Search the 1638 airfoils available in the databases filtering by name, thickness and camber. Click on an airfoil image to display a larger preview picture. There are links to the original airfoil source and dat file and the details page with polar diagrams for a range of Reynolds numbers.
(goe495-il) GOE 495 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 495 airfoil Max thickness 6.9% at 30% chord Max camber 5% at 50% chord Max Cl/Cd 126.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe264-il) GOE 264 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 264 airfoil Max thickness 6.4% at 20.2% chord Max camber 5.7% at 28.9% chord Max Cl/Cd 126.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe441-il) GOE 441 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 441 airfoil Max thickness 16% at 29.5% chord Max camber 7.7% at 39.5% chord Max Cl/Cd 126.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(stcyr24-il) St. CYR 24 (Bartel 35-IIIC) | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | St. CYR 24 (Bartel 35-IIIC) airfoil Max thickness 12.4% at 30% chord Max camber 5.9% at 40% chord Max Cl/Cd 126.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(fx05188-il) WORTMANN FX 05-188 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Wortmann FX 05-188 airfoil Max thickness 18.8% at 37.1% chord Max camber 2.6% at 50% chord Max Cl/Cd 126.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe300-il) GOE 300 (FRIEDRICHSHAFEN G20) AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 300 (Friedrichshafen G20) airfoil Max thickness 8.4% at 30% chord Max camber 6.7% at 30% chord Max Cl/Cd 126.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(goe624-il) GOE 624 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Gottingen 624 airfoil Max thickness 16% at 30% chord Max camber 5.2% at 40% chord Max Cl/Cd 126.9 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(ah81131-il) AH 81-131 | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Althaus AH 81-131 airfoil Max thickness 13.1% at 40.2% chord Max camber 2.8% at 40.2% chord Max Cl/Cd 126.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(2032c-il) 20-32C AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Dillner 20-32-C low Reynolds number airfoil Max thickness 8% at 20% chord Max camber 6.9% at 40% chord Max Cl/Cd 126.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
(e584-il) EPPLER 584 AIRFOIL | Airfoil details Send to airfoil plotter Add to comparison Lednicer format dat file Selig format dat file Source dat file | |
 | Eppler E584 sailplane airfoil Max thickness 16.6% at 38.3% chord Max camber 4.5% at 38.3% chord Max Cl/Cd 126.8 at Re# 1,000,000 Source UIUC Airfoil Coordinates Database | |
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